Kazan Helicopters Mi-17-1V Flight Manual page 20

M,,·17·1B. Flight manual
Table
1.3
Fuel Used, Distance and Time at Takeoff and Climb.
E N IP nqrne
orma ower
Takeoff weiqht, kQ
Altitude, m
11100 13000
Fuel used, Distance, Time,
Fuel used, Distance, Time,
Gte, ko Le,km t
e ,
min
Gte, kQ
Le,km t, min
Takeoff,
acceleration,
15 1 15 1
establtshino of steady climb
-
-
100
20
-
1,5
20
-
1
500 25
-
2 30
-
2
1000 35 4,0 2,5 40 5 3
2000 55 7,0 4,0 70
10 5,5
3000 75 10 6,0 100 15 8
3500
- - -
- -
11,5
4000 95 15 7,5 140 30
11,5
4800
- - -
215 40 18,0
5000 115 20 9,5
-
-
-
6000 170 30 15
-
-
-
GLF - fuel used for glide, deceleration, hovering and landing (derived from
Table
1.4).
RF- reserve fuel (for possible deviation from the selected route, variation of
weather conditions, etc.). In each specific case the reserve fuel is determined
by the Captain. In the present calculation the reserve fuel is assumed to be
equal to 5
%
of the fuel filled.
UF - unusable fuel equal to 20 kg.
Table
1.4
d L d'
d Ti . D
FlU d D' t ue se ,
IS
ance an
une m
escen an an
InQ
Descentinitiation altitude, m lAS,
Vertical speed of
Fuel Distance, Time,
km/h descent, m/s used.kq km min
Deceleration, hovering and
-
15
-
1
landinc
100
130 2t04 20 - 2
500 130
5 to 6
25 5 3
1000
140 5 to 6 30 10 4
2000 140 5to 6 45 20 7
3000
140 5t06 60 30
11
4000 120 3 t04 90 40 17
5000
120 3 to 4 130
55 25
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